National Aeronautical Establishment (Canada)

• Analysis of Flight Loads During Low-Altitude Pipeline Patrol Operations. Final Report
• Bibliography on determination of supersonic dynamic stability derivatives
• Closed Form, Finite Element Solutions For Plate Vibrations
• Guide to the laboratories of the Division of Mechanical Engineering, National Research Council and of the National Aeronautical Establishment, Ottawa, Canada
• Instrumentation of an rb-57F to Measure High-Altitude Turbulence Encounters
• Interpretation of X-Ray Powder Diffraction Patterns From Multiphase Materials
• Publications of the National Aeronautical Establishment; supplement
• The NAE high Reynolds number 15" x 60" 2-dimensional test facility